View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39439U 13066Z 23089.86698547 .00014672 00000-0 15462-2 0 9999
2 39439 97.6732 57.7762 0058038 174.1415 186.0494 14.88177764505662
| Epoch (UTC): | 30 March 2023 20:48:27 |
| Eccentricity: | 0.0058038 |
| inclination: | 97.6732° |
| perigee height: | 563 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 57.7762° |
| argument of perigee: | 174.1415° |
| revolutions per day: | 14.88177764 |
| mean anomaly at epoch: | 186.0494° |
| orbit number at epoch: | 50566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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